留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

软管锥套式空中加油系统建模与特性分析

王海涛 董新民 窦和锋 薛建平

王海涛, 董新民, 窦和锋, 等 . 软管锥套式空中加油系统建模与特性分析[J]. 北京航空航天大学学报, 2014, 40(1): 92-98.
引用本文: 王海涛, 董新民, 窦和锋, 等 . 软管锥套式空中加油系统建模与特性分析[J]. 北京航空航天大学学报, 2014, 40(1): 92-98.
Wang Haitao, Dong Xinmin, Dou Hefeng, et al. Dynamic modeling and characteristics analysis of hose-paradrogue aerial refueling system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(1): 92-98. (in Chinese)
Citation: Wang Haitao, Dong Xinmin, Dou Hefeng, et al. Dynamic modeling and characteristics analysis of hose-paradrogue aerial refueling system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(1): 92-98. (in Chinese)

软管锥套式空中加油系统建模与特性分析

基金项目: 航空科学基金资助项目(2008ZC01006)
详细信息
  • 中图分类号: V212.1

Dynamic modeling and characteristics analysis of hose-paradrogue aerial refueling system

  • 摘要: 针对自主空中加油研究中软管锥套运动模型过于简化,现有建模方法又存在成本高、计算量大、软管长度恒定等缺陷的问题,根据集中参数法原理,提出了一种长度可变的多级串联理想单摆系软管锥套运动模型.同时考虑软管收放、加油机牵连运动、重力、定常流、大气扰动、加油机尾流等内外部因素,推导了迭代形式的变长度软管锥套三维运动方程.由摆长约束导出了求解软管拉力的代数线性方程组,进而给出了模型稳定性证明和适用条件.通过数值仿真,测试了锥套阻力、平衡位置、软管收放等稳态特性,分析了加油机滚转运动、尾涡流场对软管锥套的动态影响以及软管甩鞭现象的产生机理.数值仿真结果验证了所建模型的有效性.

     

  • [1] 董新民, 徐跃鉴, 陈博.自动空中加油技术研究进展与关键问题[J].空军工程大学学报:自然科学版, 2008, 9(6):1-5 Dong Xinmin, Xu Yuejian, Chen Bo.Progress and challenges in automatic aerial refueling[J].Journal of Air Force Engineering University:Natural Science Edition, 2008, 9(6):1-5(in Chinese)
    [2] Tandale M D, Bowers R, Valasek J.Trajectory tracking controller for vision-based probe and drogue autonomous aerial refueling[J].Journal of Guidance Control and Dynamics, 2006, 29(4):846-857
    [3] 王宏伦, 杜熠, 盖文东.无人机自动空中加油精确对接控制[J].北京航空航天大学学报, 2011, 37(7):822-826 Wang Honglun, Du Yi, Gai Wendong.Precise docking control in unmanned aircraft vehicle automated aerial refueling[J].Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(7) :822-826(in Chinese)
    [4] Vassberg J C, Yeh D T, Blair A J, et al.Numerical simulations of KC-10 wing-mount aerial refueling hose-drogue dynamics with a reel take-up system[C]//21st Applied Aerodynamics Conference.Orlando:AIAA, 2003:1-22
    [5] Ro K, Basaran E, Kamman J W.Aerodynamic characteristics of paradrogue assembly in an aerial refueling system[J].Journal of Aircraft, 2007, 44(3):963-970
    [6] Vachon M J, Ray R J.Calculated drag of an aerial refueling assembly through airplane performance analysis[C]//42nd AIAA Aerospace Sciences Meeting.Reno:AIAA, 2004:1-18
    [7] Zhu Zhenghong, Meguid S A.Modeling and simulation of aerial refueling by finite element method[J].International Journal of Solids and Structures, 2007, 44:8057-8073
    [8] Ribbens W B, Saggio F, Wierenga R, et a1.Dynamics modeling of an aerial refueling hose & drogue system[C]//25th Applied Aerodynamics Conference.Miami:AIAA, 2007:1-10
    [9] Ro K, Kamman J W.Modeling and simulation of hose-paradrogue aerial refueling systems[J].Guidance Control and Dynamics, 2010, 33(1):53-63
    [10] 胡孟权, 柳平, 聂鑫, 等.大气紊流对空中加油软管锥套运动的影响[J].飞行力学, 2010, 28(5):20-23 Hu Mengquan, Liu Ping, Nie Xin, et al.Influence of air turbulence on the movement of hose-drogue[J].Flight Dynamics, 2010, 28(5):20-23(in Chinese)
    [11] 张雷雨, 张洪, 杨洋, 等.空中加油对接过程的动力学建模与仿真[J].航空学报, 2012, 33(7):1347-1354 Zhang Leiyu, Zhang Hong, Yang Yang, et al.Dynamics modeling and simulation of docking process in aerial Refueling[J].Acta Aeronautica et Astronautica Sinica, 2012, 33(7):1347-1354(in Chinese)
    [12] 陈博, 董新民, 徐跃鉴, 等.加油机尾流场建模及受油机飞行安全性分析[J].系统仿真学报, 2008, 20(8):1994-2002 Chen Bo, Dong Xinmin, Xu Yuejian, et al.Modeling of tanker's wake field and flight safety analysis of receiver aircraft[J].Journal of System Simulation, 2008, 20(8):1994-2002(in Chinese)
  • 加载中
计量
  • 文章访问数:  1913
  • HTML全文浏览量:  192
  • PDF下载量:  669
  • 被引次数: 0
出版历程
  • 收稿日期:  2013-03-15
  • 网络出版日期:  2014-01-20

目录

    /

    返回文章
    返回
    常见问答